Paparazzi UAS
v5.0.5_stable7g4b8bbb7
Paparazzi is a free software Unmanned Aircraft System.

Fixed wing horizontal adaptive control. More...
Go to the source code of this file.
Macros  
#define  H_CTL_ROLL_SUM_ERR_MAX (MAX_PPRZ/2.) 
#define  H_CTL_PITCH_SUM_ERR_MAX (MAX_PPRZ/2.) 
#define  stabilization_adaptive_SetRollIGain(_gain) 
#define  stabilization_adaptive_SetPitchIGain(_gain) 
Variables  
float  h_ctl_roll_sum_err 
float  h_ctl_pitch_sum_err 
float  h_ctl_roll_igain 
float  h_ctl_pitch_igain 
float  h_ctl_roll_Kffa 
float  h_ctl_roll_Kffd 
float  h_ctl_pitch_Kffa 
float  h_ctl_pitch_Kffd 
float  h_ctl_pitch_of_roll 
float  h_ctl_ref_roll_angle 
float  h_ctl_ref_roll_rate 
float  h_ctl_ref_roll_accel 
float  h_ctl_ref_pitch_angle 
float  h_ctl_ref_pitch_rate 
float  h_ctl_ref_pitch_accel 
bool_t  use_airspeed_ratio 
Fixed wing horizontal adaptive control.
Definition in file stabilization_adaptive.h.
#define H_CTL_PITCH_SUM_ERR_MAX (MAX_PPRZ/2.) 
Definition at line 48 of file stabilization_adaptive.h.
Referenced by h_ctl_pitch_loop().
#define H_CTL_ROLL_SUM_ERR_MAX (MAX_PPRZ/2.) 
Definition at line 47 of file stabilization_adaptive.h.
Referenced by h_ctl_roll_loop().
#define stabilization_adaptive_SetPitchIGain  (  _gain  ) 
Definition at line 55 of file stabilization_adaptive.h.
#define stabilization_adaptive_SetRollIGain  (  _gain  ) 
Definition at line 50 of file stabilization_adaptive.h.
float h_ctl_pitch_igain 
Definition at line 86 of file stabilization_adaptive.c.
Referenced by h_ctl_init(), and h_ctl_pitch_loop().
float h_ctl_pitch_Kffa 
Definition at line 88 of file stabilization_adaptive.c.
Referenced by h_ctl_init(), and h_ctl_pitch_loop().
float h_ctl_pitch_Kffd 
Definition at line 89 of file stabilization_adaptive.c.
Referenced by h_ctl_init(), and h_ctl_pitch_loop().
float h_ctl_pitch_of_roll 
Definition at line 95 of file stabilization_adaptive.c.
Referenced by h_ctl_init(), and h_ctl_pitch_loop().
float h_ctl_pitch_sum_err 
Definition at line 87 of file stabilization_adaptive.c.
Referenced by h_ctl_init(), and h_ctl_pitch_loop().
float h_ctl_ref_pitch_accel 
Definition at line 60 of file stabilization_adaptive.c.
Referenced by h_ctl_pitch_loop().
float h_ctl_ref_pitch_angle 
Definition at line 58 of file stabilization_adaptive.c.
Referenced by h_ctl_pitch_loop().
float h_ctl_ref_pitch_rate 
Definition at line 59 of file stabilization_adaptive.c.
Referenced by h_ctl_pitch_loop().
float h_ctl_ref_roll_accel 
Definition at line 57 of file stabilization_adaptive.c.
Referenced by h_ctl_roll_loop().
float h_ctl_ref_roll_angle 
Definition at line 55 of file stabilization_adaptive.c.
Referenced by h_ctl_roll_loop().
float h_ctl_ref_roll_rate 
Definition at line 56 of file stabilization_adaptive.c.
Referenced by h_ctl_roll_loop().
float h_ctl_roll_igain 
Definition at line 72 of file stabilization_adaptive.c.
Referenced by h_ctl_init(), and h_ctl_roll_loop().
float h_ctl_roll_Kffa 
Definition at line 74 of file stabilization_adaptive.c.
Referenced by h_ctl_init(), and h_ctl_roll_loop().
float h_ctl_roll_Kffd 
Definition at line 75 of file stabilization_adaptive.c.
Referenced by h_ctl_init(), and h_ctl_roll_loop().
float h_ctl_roll_sum_err 
Definition at line 73 of file stabilization_adaptive.c.
Referenced by h_ctl_init(), and h_ctl_roll_loop().
bool_t use_airspeed_ratio 
Definition at line 97 of file stabilization_adaptive.c.
Referenced by h_ctl_init().